Acoustic Characteristics of Orifice Holes Exposed to Grazing Flow
スポンサーリンク
概要
- 論文の詳細を見る
Experimental and theoretical studies were conducted on the acoustic characteristics of orifice holes exposed to a grazing flow. The impedance tube method was applied and the grazing flow was given by an open jet to avoid standing wave effects in the radiation field. The radiation resistance was found to become negative at specific conditions determined by flow Mach number, frequency and hole diameter. The open area ratio of orifice holes was pointed out to have a stronger influence on the impedance than considered. The concept of ' constant volume flow through orifice hole' is not necessarily valid. A potential flow theory was presented on the radiation impedance of a tube opening exposed to a grazing flow. In the theory the flow region and the tube region were connected to satisfy the coincidence conditions of displacement and pressure at the opening. This theory was found to predict fairly well the various aspects of impedance obtained in the experiments.
- 一般社団法人日本機械学会の論文
著者
-
Kaji Shojiro
Department Of Aeronautics And Astronautics University Of Tokyo
-
Okazaki Takuro
Faculty Of Engineering University Of Tokyo
-
Okazaki Takuro
Faculty Of Industrial Engineering Nihon University
-
HIRAMOTO Masaaki
Department of Aeronautics, University of Tokyo
-
Kaji Shojiro
Department Of Aeronautics And Astronautics Faculty Of Engineering The University Of Tokyo
-
Hiramoto Masaaki
Department Of Aeronautics University Of Tokyo
関連論文
- Jet Noise : Far Noise Field of Subsonic Free Air Jet
- The Effects of Aspect Ratio of a Finite Length Slit on the Mixing in the Three-Dimensional Supersonic Flow
- Jet Noise : 3rd Report, Effect of the Shape of Nozzle-Exit
- Jet Noise : 2nd Report, Effect of Shear on the Noise of a Jet
- Stall-Flutter in Cascade : 2nd Report, Translatory Vibration of Cascade Blades as Treated by Semi-Actuator Disc Method, Part 2
- Stall-Flutter in Cascade : 3rd Report, Arbitrary Mode Vibration of Cascade Blades as Treated by Semi-Actuator Disc Method
- Acoustic Characteristics of Orifice Holes Exposed to Grazing Flow
- Stall-Flutter in Cascade : 1st Report, Translatory Vibration of Cascade Blades as Treated by Semi-Actuator Disc Method, Part 1
- The Two-Dimensional Supersonic Flow and Mixing Field with a Perpendicular Injection
- Study on the Swirling Flow Field in a Rotating Cylinder : Numerical Analysis
- Study of Transonic Cascade Airfoils by a Panel Method : Series B : Fluids Engineering, Heat Transfer, Combustion, Power, Thermophysical Properties
- Theoretical Study on the Unsteady Aerodynamic Characteristics of an Oscillating Cascade with Tip Clearance (In the Case of a Nonloaded Cascade)
- Theoretical Study on the Unsteady Aerodynamic Characteristics of an Oscillating Cascade with Tip Clearance : In the Case of Loaded Cascade
- Experimental Study on Unsteady Aerodynamic Characteristics of an Oscillating Cascade with Tip Clearance
- The Injection Methods and Mixing Characteristics in the Two-Dimensional Supersonic Free Stream
- The Three-Dimensional Supersonic Flow and Mixing Fields with a Perpendicular Air Injection from a Finite Length Slit
- The Effects of Acoustically Lined Walls on Cascade Flutter